Non-planarity to improve subsonic performance of delta wing at low angle of attack

Keyphrases

• Low Angle 100%
• Non-planarity 100%
• Angle of Attack 100%
• Delta Wing 100%
• X-configuration 66%
• Lift Generation 66%
• Load Balancing 33%
• Flap 33%
• High Aspect Ratio Wing 33%
• Solution Feature 33%
• Static Pressure Measurement 33%
• Feature Surface 33%
• Leading Edge Vortex 33%
• High-lift 33%
• Subsonic Speed 33%
• Vortex Trapping 33%

Engineering

• Angle-of-Attack 100%
• Delta Wing 100%
• Vortex 33%
• Flaps 33%
• Surface Feature 33%
• Leading Edge Vortex 33%
• Static Pressure Measurement 33%
• Load Balance 33%
• High Aspect Ratio 33%
• Subsonic Speed 33%